1、IEEE Std 292-1969(R2005)Errata to IEEE Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate GyrosSponsorGyro and Accelerometer Panelof theIEEE Aerospace and Electronic Systems SocietyCorrection SheetIssued 26 April 2010Copyright 2010 by the Institute of Electrical and Electronics
2、 Engineers, Inc. All rights reserved. Published 2010.Printed in the United States of America.This correction sheet may be freely reproduced and distributed in order to maintain the utility and currency of theunderlying Standard. This correction sheet may not be sold, licensed or otherwise distribute
3、d for any commercialpurposes whatsoever. The content of this correction sheet may not be modified. Correction Sheet to IEEE Std 292-1969STDPD16014 26 April 2010Page 11, 3.3.14 Zero Offset should be corrected to read as follows:_ g113/s max.Page 11, 3.3.15 Zero Acceleration-Sensitive Drift Rate shoul
4、d be corrected to read as follows:_ (g113/s)/g max._ (g113/s)/g2max.Page 12, 3.3.19 Angular Acceleration Sensitivity About the Output Axis should be corrected to read asfollows:_ (g113/s)/(rad/s2) max.Page 17, 3.6.4.2 Vibration should be corrected to read as follows:Sinusoidal: _ in double amplitude
5、 (DA) _ to _ hertz; _ g peak, _ to _ hertz.Sweep rate shall be _ minutes per octave (continuous). Exposure shall be _ minutes per axis.Page 26, 6.3 Model Equation, the first Equation should be corrected to read as follows:= (effect of case rotation about the IRA)g16s(g840+ g1430) (effect of case rot
6、ation about the SRA)+0g143sg16 (J/H)0(effect of case rotation about the axis perpendicular to theIRA and SRA)+ D0(acceleration-insensitive drift rate)+ D1iai+ D1sas(acceleration-sensitive drift rate)+ D2aias(acceleration-squared-sensitive drift rate)+ Kti (command rate)Page 26, 6.3 Model Equation, i
7、n the where list, the g1430and g143sdescription should be corrected to readas follows:g1430= Misalignment angle between the plane containing SRA and the axis perpendicular toIRA and SRA, and the plane containing SA and the axis perpendicular to IRA and SRA,wheni= 0= s= 0. It is approximately equal t
8、o D0g16 (Kr/H + ?dcl256?s) g8401/s.g143s= Misalignment angle between the plane containing SA and the axis perpendicular toIRA and SRA, and the plane containing SA and OA. It is approximately equal to (Ks/H)g840g16 D01/0.Axes shall be defined.When available, supply the specific vibration versus frequency for the application.If exposure to random vibration is required, power spectral density, bandwidth, peak acceleration level,and duration shall be specified.JH- g840CH- g840KrH- g840+g77ig77g77g77g77g77g77g77g77
